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Journal Articles
Alloy Digest (1980) 29 (9): Sn-10.
Published: 01 September 1980
... and recycled into new uses any number of times. Among its many uses are fusible mandrels for electroforming, proof casting in foundries, low-temperature solder, holding jet engine blades for machining and dies for wax patterns for investment casting. This datasheet provides information on composition, physical...
Journal Articles
Alloy Digest (1980) 29 (11): Bi-20.
Published: 01 November 1980
... jet engine blades for machining and broaching, support for bending tubing and extrusions and seals for annealing and nitriding furnaces. This datasheet provides information on composition, physical properties, hardness, and tensile properties. It also includes information on casting, forming, heat...
Journal Articles
Alloy Digest (1986) 35 (11): SS-478.
Published: 01 November 1986
... AISI No. 651 is an austenitic iron-base superalloy with a relatively high ratio of strength to alloying element content. It is capable of withstanding high static and dynamic stresses through at least 1200 F. It is used for various high-temperature applications such as components for jet engines...
Journal Articles
Alloy Digest (1998) 47 (6): SS-719.
Published: 01 June 1998
... Allegheny Ludlum Type 310 is an austenitic chromium-nickel steel with high heat resisting properties. It is recommended for furnace equipment, heat treating boxes, burners, heat recovery systems, jet engine components, and heat exchangers. This datasheet provides information on composition...
Journal Articles
Alloy Digest (1998) 47 (12): Re-2.
Published: 01 December 1998
... Pure rhenium is used in electronic applications, as filler wire in welding, and as an alloying addition to superalloys used in jet engines. This datasheet provides information on composition, physical properties, and microstructure. It also includes information on corrosion resistance as well...
Journal Articles
Alloy Digest (1999) 48 (3): SA-498.
Published: 01 March 1999
... Lescalloy 6305 VAC-ARC steel is a modified AISI 4140 steel with higher molybdenum content and additional vanadium. The alloy is most frequently used in the quenched and tempered condition. Jet engine shafting is a typical application. This datasheet provides information on composition, physical...
Journal Articles
Alloy Digest (2002) 51 (4): SS-851.
Published: 01 April 2002
... Crucible A-286 is an age-hardenable austenitic Fe-Ni-Cr alloy designed for service up to 704 deg C (1300 deg F) on jobs requiring high strength and good corrosion resistance at the operating temperature. The alloy offers high ductility in notched sections. Crucible A-286 is used in jet engines...
Journal Articles
Alloy Digest (2002) 51 (5): SS-853.
Published: 01 May 2002
... and improves weldability. Typical uses include furnace parts, heating elements, aircraft and jet engine parts, heat exchangers, carburizing-annealing boxes, sulfite liquor handling equipment, kiln liners, boiler baffles, refinery and chemical processing equipment, and auto exhaust parts. This datasheet...
Journal Articles
Alloy Digest (1967) 16 (9): Ni-127.
Published: 01 September 1967
... CM-R41 is a vacuum-melted, precipitation hardening nickel-base alloy possessing outstanding properties in the temperature range of 1200 F to 1800 F. It is recommended for jet engine and gas turbine components operating at high temperatures. This datasheet provides information on composition...
Journal Articles
Alloy Digest (1967) 16 (9): SS-200.
Published: 01 September 1967
... AISI No. 616 is a hardenable martensitic type stainless steel recommended for high temperature applications up to 1200 F. It is used for steam turbine blades and buckets, valves, jet engine components, and high temperature bolting. This datasheet provides information on composition, physical...
Journal Articles
Alloy Digest (1968) 17 (2): SA-222.
Published: 01 February 1968
... AISI No 602 is a low-alloy high-temperature constructional steel of the Cr-Mo-V-Si type that possesses useful strength after suitable heat treatment at temperatures up to 1000 F. It is used for jet engine compressor wheels and blading. This datasheet provides information on composition, physical...
Journal Articles
Alloy Digest (1968) 17 (2): Ni-131.
Published: 01 February 1968
... GMR-235 Alloy is a nickel-base, precipitation-hardening alloy available in investment cast form for high temperature service. It is recommended for gas turbine and jet engine components operating in excess of 1400 F. This datasheet provides information on composition, physical properties, hardness...
Journal Articles
Alloy Digest (1968) 17 (8): SS-212.
Published: 01 August 1968
... CMN-155 is an austenitic iron-base alloy having high oxidation and heat resistance combined with good high temperature properties. It is recommended for jet engine and gas turbine components, high temperature fasteners, and rocket chambers. This datasheet provides information on composition...
Journal Articles
Alloy Digest (1970) 19 (1): Co-60.
Published: 01 January 1970
... CML-605 is a cobalt-base alloy having high strength, heat and oxidation resistance at elevated temperatures above 1600 F. It is recommended for gas turbine and jet engine components operating in the 1600 to 2000 F temperature range. This datasheet provides information on composition, physical...
Journal Articles
Alloy Digest (1970) 19 (2): Ni-150.
Published: 01 February 1970
... processing equipment, reaction vessels, valves and jet engine afterburner cones. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep. It also includes information on low and high temperature performance, and corrosion...
Journal Articles
Alloy Digest (1970) 19 (3): SA-250.
Published: 01 March 1970
... REPUBLIC RSM 250 is an 18% nickel-cobalt-molybdenum age-hardening steel designed to develop 250,000 psi yield strength with good toughness. It is recommended where a combination of strength, toughness and notch resistance is required such as aircraft landing gears and jet engine components...
Journal Articles
Alloy Digest (1970) 19 (5): Ni-153.
Published: 01 May 1970
... NIMONIC 93 is a nickel-base alloy having high elevated temperature strength, high oxidation resistance and good corrosion resistance. It is recommended for jet engine and gas turbine components. This datasheet provides information on composition, physical properties, hardness, elasticity...
Journal Articles
Alloy Digest (1953) 2 (3): Mg-4.
Published: 01 March 1953
... ELEKTRON ZT1 is distinguished by the best combination of properties at temperatures of and above 600 F of any magnesium casting alloy; also by excellent room temperature properties, by freedom from microporosity, and exceptionally good founding characteristics. Very suitable for jet engine parts...
Journal Articles
Alloy Digest (1952) 1 (2): Mg-2.
Published: 01 October 1952
... Flylite ZRE-1 is a creep resistant magnesium-base alloy primarily designed for jet engine components and other high temperature applications. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive strength as well as creep...
Journal Articles
Alloy Digest (1962) 11 (1): Ti-32.
Published: 01 January 1962
... Ti-8A1-1Mo-1V is a titanium alloy having excellent creep resistance and stress-rupture life. It is recommended for jet engine components operating up to 900 F. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and shear strength as well...